Stability of the steady rotations of a satellite with internal damping in a central gravitational field

Q3 Mathematics

Pmm Journal of Applied Mathematics and Mechanics Pub Date : 2017-01-01 DOI:10.1016/j.jappmathmech.2017.08.002

N.I. Amelkin, V.V. Kholoshchak

引用次数: 9

Abstract

The rotational motion of a satellite in a central gravitational field in the presence of internal dissipation is studied. The satellite is modelled by a system consisting of two bodies, a shell and a spherical damper. The stability of the steady rotations is investigated for a dynamically symmetric satellite moving in a circular Kepler orbit.

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具有内阻尼的卫星在中心重力场中稳定旋转的稳定性

研究了卫星在中心重力场中存在内耗散时的旋转运动。卫星的模型是由两个物体、一个壳体和一个球形阻尼器组成的系统。研究了在圆形开普勒轨道上运动的动态对称卫星的稳定旋转的稳定性。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

Pmm Journal of Applied Mathematics and Mechanics 物理-力学

CiteScore

0.70

自引率

0.00%

发文量

审稿时长

6-12 weeks

期刊介绍： This journal is a cover to cover translation of the Russian journal Prikladnaya Matematika i Mekhanika, published by the Russian Academy of Sciences and reflecting all the major achievements of the Russian School of Mechanics.The journal is concerned with high-level mathematical investigations of modern physical and mechanical problems and reports current progress in this field. Special emphasis is placed on aeronautics and space science and such subjects as continuum mechanics, theory of elasticity, and mathematics of space flight guidance and control.